Airbus A300-600F vs. Airbus H225 Super Puma
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Airbus A300-600F |
versus |
Airbus H225 Super Puma |
54.08 m |
177 ft 5 in |
length |
14.06 m |
46 ft 2 in |
17.05 m |
55 ft 11 in |
height |
4.38 m |
14 ft 4 in |
44.84 m |
147 ft 1 in |
wingspan |
|
|
2 x General Electric CF6-80C2A5 turbofan engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
Approximately 59,000 lbf per engine |
thrust per engine |
2,778 hp |
Approximately 118,000 lbf total |
total thrust |
5,556 hp |
170,000 kg |
374,786 lb |
MTOW |
11,000 kg |
24,251 lb |
4,830 km |
2,608 nm |
range |
857 km |
463 nm |
860 km/h |
534 mph |
cruise speed |
242 km/h |
150 mph |
|
capacity |
24-28 |
|
|
rotor diameter |
16.2 m |
53 ft 2 in |
|
|
rate of climb |
10.7 m/s |
2,106 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.